Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds /

Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds / by Roger Chamberlin.

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Bibliographic Details
Online Access: Search for the full-text version of this title in HathiTrust
Main Author: Chamberlin, Roger
Corporate Authors: Lewis Research Center, United States. National Aeronautics and Space Administration
Format: Government Document Book
Language:English
Published: Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974.
Series:NASA technical memorandum ; X-3053.
Subjects:
Jet nozzles.
Airplanes > Turbojet engines.
Drag (Aerodynamics)
Aerodynamics, Transonic.
Reynolds number.
Airplanes > Nacelles.
Delta Dart (Jet fighter plane)
Description
Item Description:Cover title.
Prepared at Lewis Research Center.
Physical Description:23 pages : illustrations ; 27 cm.
Bibliography:Includes bibliographical references (pages 8-9)

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